Patents by Inventor Chris Speights

Chris Speights has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 7704056
    Abstract: A two-stage vapor cycle compressor includes a first stage impeller, a second stage impeller situated adjacent to the first stage impeller, an electric motor running on a pair of foil bearings, a thrust disk including two foil bearings and being positioned between the second stage impeller and the electric motor, and a compressor housing enclosing the first and second stage impeller and the electric motor. A refrigerant vapor compressed by the first stage and second stage impeller flows through an internal passageway formed by the compressor housing and cools the foil bearings and the electric motor. The compressor may be a gravity insensitive, small, and lightweight machine that may be easily assembled at low manufacturing costs. The two-stage vapor cycle compressor may be suitable for, but not limited to, applications in vapor compression refrigeration systems, such as air-conditioning systems, for example, in the aircraft and aerospace industries.
    Type: Grant
    Filed: September 19, 2008
    Date of Patent: April 27, 2010
    Assignee: Honeywell International Inc.
    Inventors: Mike M. Masoudipour, Allen Hansen, Chris Speights, Phung K. Duong, Zeng Qian
  • Publication number: 20090044548
    Abstract: A two-stage vapor cycle compressor includes a first stage impeller, a second stage impeller situated adjacent to the first stage impeller, an electric motor running on a pair of foil bearings, a thrust disk including two foil bearings and being positioned between the second stage impeller and the electric motor, and a compressor housing enclosing the first and second stage impeller and the electric motor. A refrigerant vapor compressed by the first stage and second stage impeller flows through an internal passageway formed by the compressor housing and cools the foil bearings and the electric motor. The compressor may be a gravity insensitive, small, and lightweight machine that may be easily assembled at low manufacturing costs. The two-stage vapor cycle compressor may be suitable for, but not limited to, applications in vapor compression refrigeration systems, such as air-conditioning systems, for example, in the aircraft and aerospace industries.
    Type: Application
    Filed: September 19, 2008
    Publication date: February 19, 2009
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: MIKE M. MASOUDIPOUR, ALLEN HANSEN, CHRIS SPEIGHTS, PHUNG K. DUONG, ZENG QIAN
  • Publication number: 20080199326
    Abstract: A two-stage vapor cycle compressor includes a first stage impeller, a second stage impeller situated adjacent to the first stage impeller, an electric motor running on a pair of foil bearings, a thrust disk including two foil bearings and being positioned between the second stage impeller and the electric motor, and a compressor housing enclosing the first and second stage impeller and the electric motor. A refrigerant vapor compressed by the first stage and second stage impeller flows through an internal passageway formed by the compressor housing and cools the foil bearings and the electric motor. The compressor may be a gravity insensitive, small, and lightweight machine that may be easily assembled at low manufacturing costs. The two-stage vapor cycle compressor may be suitable for, but not limited to, applications in vapor compression refrigeration systems, such as air-conditioning systems, for example, in the aircraft and aerospace industries.
    Type: Application
    Filed: February 21, 2007
    Publication date: August 21, 2008
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: MIKE M. MASOUDIPOUR, ALLEN HANSEN, CHRIS SPEIGHTS, PHUNG K. DUONG
  • Patent number: 7302804
    Abstract: A closed loop cooling system and method for an oil-free electric motor of an aircraft cabin air compressor. A closed-loop fan, which may be coupled to a motor rotor opposite a compressor impeller, circulates the required cooling air in a closed loop through a motor stator and bearings, a motor cooler, and a ducting used to complete the flow circuit via a ram air cooled heat exchanger. The cooling air may be pressurized to cabin pressure. The system and method of the present invention eliminates the possibility of contaminating trace amounts of oil in cabin supply air.
    Type: Grant
    Filed: April 5, 2004
    Date of Patent: December 4, 2007
    Assignee: Honeywell International, Inc.
    Inventors: Roger P. Murry, Chris Speights
  • Publication number: 20040261428
    Abstract: A closed loop cooling system and method for an oil-free electric motor of an aircraft cabin air compressor. A closed-loop fan, which may be coupled to a motor rotor opposite a compressor impeller, circulates the required cooling air in a closed loop through a motor stator and bearings, a motor cooler, and a ducting used to complete the flow circuit via a ram air cooled heat exchanger. The cooling air may be pressurized to cabin pressure. The system and method of the present invention eliminates the possibility of contaminating trace amounts of oil in cabin supply air.
    Type: Application
    Filed: April 5, 2004
    Publication date: December 30, 2004
    Applicant: Honeywell International Inc.
    Inventors: Roger P. Murry, Chris Speights